[0001] This invention relates to a method of manufacturing a prepreg in which reinforcing
fibers are impregnated with a matrix resin and particularly to a prepreg manufacturing
method suitable for production of a thick prepreg.
[0002] Presently, fiber reinforced composite materials in which reinforcing fibers are hardened
together with a matrix resin, have been widely used in various technical fields such
as automobiles, airplanes, building materials, sporting goods, etc. Prepregs have
extensively been used for manufacturing such fiber reinforced composite material products.
[0003] Such a prepreg consists of a flexible sheet in which a fiber reinforced composite
resin layer having reinforcing fibers impregnated with a matrix resin is formed in
a thin layer on a release paper as a support and then the matrix resin is partially
cured in advance. The prepreg in which reinforcing fibers are preliminarily impregnated
with the matrix resin, is covered with a cover film thereon to make it a product,
and is stored for later use.
[0004] In order to produce the fiber reinforced composite material product by using the
prepreg, a desired number of the prepeg sheets may for example be laminated on a mould
or model. The prepreg laminates are subjected to pressing and heating not only to
shape them but also to cure the matrix with the result that the composite material
product is easily obtained.
[0005] Heretofore, such a prepreg has been manufactured in the following process.
[0006] A unidirectional fiber reinforced prepreg will be described by way of example. A
matrix resin is coated on a first release paper. The first release paper coated with
the matrix resin and a second release paper on which there is no matrix resin coat,
are successively fed in between a pair of rollers, and simultaneously reinforcing
fibers are successively supplied in the longitudinal direction of the fibers in between
the rollers covering the width of the release paper. The first and second release
papers are superimposed and pressed together in such a manner that the reinforcing
fibers are unidirectionally arranged on the matrix resin layer. Subsequently, the
reinforcing fibers and the matrix resin layer are pressed and heated at a following
press and heat section where press rollers and a hot plate are disposed, so that the
reinforcing fibers are forced into the matrix resin layer and impregnated with the
matrix resin. Simultaneousuly, the resin is partially cured. Thus, a unidirectional
fiber reinforced prepreg is obtained, in which the reinforcing fibers, unidirectionally
arranged, are impregnated with the matrix resin. The obtained prepreg is taken up
on roller after separating the second release paper from the prepreg and then applying
a cover film onto the prepreg to make it a product.
[0007] Alternatively, the second release paper, in addition to the first release paper,
is coated with the matrix resin. A unidirectional fiber reinforced prepreg in which
the reinforcing fibers, unidirectionally arranged, are impregnated with the matrix
resin, is obtained by using the first and second release papers coated with the matrix
resin, and impregnating reinforcing fibers with the matrix resin and then partially
curing the resin according to the process described above. Similarly, the obtained
prepreg is taken up on a roller after separating one of the release papers from the
prepreg and applying a cover film onto the prepreg to make it a product.
[0008] On the other hand it is required that the matrix resin should be coated on the release
paper in a uniform thickness. Further, from the viewpoint of operation efficiency
in uniformly coating the matrix resin it is required that the matrix resin should
have a viscosity in a predetermined low viscosity range Vis, for example, a viscosity
between 2,000 to 20,000 mPa.s (centipoise) during coating operation, as shown in Fig.
5 which schematically shows a viscosity-temperature property of the matrix resin.
Particularly, such things are strongly required in the case where the matrix resin
is thickly coated to manufacture a thick prepreg.
[0009] Formerly, the matrix resin, however, has to be used at a high temperature Ta, for
instance, at a temperature between 100 and 110 °C in order to conduct coating operation
in the predetermined viscosity range Vis since the viscosity of the matrix resin used
is relatively high. This increases the constructural burden of resin temperature maintaining
means of the coating system.
[0010] Therefore, attempts have been made to conduct coating by using the matrix resin which
has a relatively low viscosity, the property of which is shown by the straight line
B. In this case, the viscosity range Vis for coating opreration can easily be obtained
even if the temperature of the resin is reduced from the temperature Ta to a relatively
low temperature Tb, for instance, a temperature between 70 and 80 °C.
[0011] According to that process, the construction of the resin temperature maintaining
means of the coating system is easier. A further benefit is that in the obtained prepreg
the reinforcing fibers are sufficiently and very uniformly impregnated with the matrix
resin since the matrix resin itself has a low viscosity.
[0012] However, even if the matrix resin layer into which the reinforcing fibers are embedded
is partially cured after the reinforcing fibers are impregnated with the matrix resin,
the matrix resin layer exhibits a lower viscosity to the extent that the relatively
low viscosity matrix resin is used. Therefore, the matrix resin layer of the prepreg
is sticky, so that the cover film applied to the resin layer adheres to the same.
This is disadvantageous for when the fiber reinforced composite material is manufactured,
it is difficult to separate the cover film, resulting in interfering with the use
thereof.
[0013] An object of the invention is to provide a method of manufacturing a prepreg which
can be used for production of fiber reinforced composite materials by depriving a
matrix layer with reinforcing fibers of tackiness, preventing a cover film applied
onto thematrix layer from adhering to the same, and facilitating the separation of
the cover film therefrom.
[0014] The above-mentioned object can be accomplished by a method of manufacturing a prepreg
in accordance with the present invention. In brief, this invention is a method of
manufacturing a prepreg, which comprises coating a release paper with a matrix resin
having a low viscosity, supplying reinforcing fibers in between the paper coated with
the matrix resin and a release paper with no coat of the matrix resin, impregnating
the reinforcing fibers with the matrix resin by heating and pressing the papers while
arranging the reinforcing fibers on the matrix resin layer. Subsequently, after separating
one of the papers, a room-temperature curing type hardener is coated on a surface
of the matrix resin layer to weakly harden the surface of the matrix resin layer.
Thereafter, a cover film is laid onto the matrix resin layer.
[0015] According to another embodiment of the present invention, in place of said release
paper with no coat of the matrix resin, a release paper which is coated with a low
viscosity matrix resin like said matrix resincoated release paper may be employed.
In this case, a prepreg may be manufactured in the same method as that described above.
Further, instead of using a release paper to be coated with a low viscosity matrix
resin, as described above, a resin-coated paper, in which a low viscosity matrix resin
layer was formed on a release paper in advance, may be used.
[0016] The invention will now be described by way of example only with reference to the
accompanying drawings in which:
Fig. 1 is a explanatory view showing an embodiment of a prepreg manufacturing method
according to the present invention;
Fig. 2 is a sectional view of a prepreg manufactured by the method of Fig. 1;
Fig. 3 is a explanatory view showing another embodiment of a prepreg manufacturing
method according to the present invention;
Fig. 4 is a explanatory view showing a further embodiment of a prepreg manufacturing
method according to the present invention; and
Fig. 5 is a graph schematically showing a temperature-viscosity relationship of the
matrix resin.
[0017] Fig. 1 is an explanatory view showing an embodiment of a prepreg manufacturing method
according to the present invention. Fig. 2 is a sectional view showing a prepreg obtained
by present method. The prepreg manufactured by the present method comprises a release
paper 1 and a low viscosity matrix resin layer 2 containing reinforcing fibers 4 formed
on the release paper 1, as shown in Fig. 2. The matrix resin layer 2 is covered with
a cover film 3. The surface layer of the matrix resin layer 2 is a high viscosity
layer 2a.
[0018] A manufacturing method of the present invention will be described. As shown in Fig.
1, a roll coater 10 is disposed on the upstream side of a line for manufacturing a
prepreg. A matrix resin 2' is applied by the roll coater 10 onto a first release paper
1 successively supplied from a release paper roller not shown.
[0019] According to the present invention, the matrix resin 2' has been prepared such as
to have a low viscosity, so that even if a thick coat of the matrix resin 2' on the
release paper 1 is required, the coating can uniformly be conducted. Moreover, and
the reinforcing fibers 4 can sufficiently and uniformly be impregnated with the matrix
resin by heating and pressing during the impregnation of the matrix resin.
[0020] As for the matrix resin 2', a thermosetting matrix resin such as an epoxy resin,
an unsaturated polyester resin, a polyurethane resin, a diallyl phthalate resin, and
a phenolic resin may be employed. The matrix resin has a viscosity of 2,000 to 20,000
mPa.s at a coating temperature of 70 °C , for example. A curing agent and a curing
accelerator are suitably added such that the curing temperature ranges from 50 to
200°C . Moreover, other additives such as an flexibilizer, etc. may be employed.
[0021] Citing a preferable example of the matrix resin, an epoxy resin is preferable as
the matrix resin. And, one or several of the following epoxy resins are selected for
usable matrix resins: for example, (1) a glycidyl ether epoxy resin (bisphenol A,
F, S epoxy resin, novolac epoxy resin and brominated bisphenol A epoxy resin); (2)
a cyclic aliphatic epoxy resin; (3) a glycidyl ester epoxy resin; (4) a glycidyl amine
epoxy resin; (5) a hetero-cyclic epoxy resin; and various other epoxy resins. In particular,
bisphenol A, F, S glycidyl amine epoxy resin is suitably used.
[0022] As for the curing agent, an amine curing agent such as dicyandiamide (DICY), diaminophenylsulfone
(DDS), and diaminodiphenylmethane (DDM); and an acidic anhydride such as hexahydrophthalic
anhydride (HHPA), methylhexahydrophthalic anhydride (MHHPA), etc. may be employed,
and particularly, the amine curing agent is suitably used.
[0023] As for the curing accelerator, imidazole, boric acid ester, Lewis acid, organometallic
compound, DCMU, etc. are cited.
[0024] Although the thickness of the matrix resin 2' depends on the thickness of the prepreg
to be manufactured, the thickness of the matrix resin 2' ranges from 5 to 200 µm,
in general, and from 200 to 300 µm for a thick pregpreg.
[0025] The first release paper 1 having the marix resin layer 2 formed with the resin 2'
is fed in between a pair of press rollers 11 disposed on the manufacturing line. Concurrently
with this, the reinforcing fibers 4 are successively supplied in the longitudinal
direction of the fibers from a fiber supply roller not shown in between the pair of
press rollers 11 covering the width of the release paper 1 so that the reinforcing
fibers 4 are laid over the matrix resin layer while arranging the fibers in one direction.
Moreover, a second release paper 5, which is not coated with the matrix resin, is
supplied from a release paper supply roller not shown onto the fibers 4 and laid over
the same. The first release paper 1, the reinforcing fibers 4 and the second release
paper 5 are then pressed together by the press rollers 11.
[0026] As the reinforcing fibers 4, inorganic fibers such as carbon fibers, boron fibers,
glass fibers, alumina fibers, silicon carbide fibers and silicon nitride fibers; organic
fibers such as aramid fibers, polyarylate fibers and polyethylene fibers; or metal
fibers such as titanium fibers, amorphous fibers and stainless steel fibers may optionally
be used. These fibers may be used independently or as hybrid fibers obtained by combining
the fibers.
[0027] Subsequently, the reinforcing fibers 4 are forced into the matrix resin layer 2 to
impregnate the fibers 4 with the matrix resin 2 by pressing and heating the reinforcing
fibers 4 and the matrix resin layer 2 from the upper and the lower sides thereof at
the following heat and press section where a plurality of press rollers 12 and a hot
plate 13 facing the rollers are disposed. Simultaneously, the resin 2' is partially
cured to thereby obtain a prepreg in which the reinforcing fibers are unidirectionally
arranged.
[0028] During this impregnation the resin 2' can sufficiently and uniformly be impregnated
into the reinforcing fibers 4 by heating and pressing, resulting in producing a good
quality prepreg, since the matrix resin layer 2 is formed of the resin 2' having a
low viscosity. However, as the low viscosity matrix resin 2' is employed, the viscosity
of the matrix resin 2' is still low after being partially cured, so that the matrix
resin layer 2 with the reinforcing fibers 4 is sticky. Therefore, in that state, if
the cover film 3 is applied to the matrix resin layer 2, the cover film 3 adheres
to the matrix resin layer 2.
[0029] According to the present invention, after the second release paper 5 is separated
by means of a take-up roller 14, a room-temperature curing type hardener 6 is coated
on the prepreg downstream of the release paper separation section by means of a spray
coater 15 with the result that the surface layer of the matrix resin layer 2 is weakly
hardened to form a high viscosity layer 2a.
[0030] As for the room-temperature curing type hardener, aromatic amine, polyamine, etc.
may be employed. These curing agents complete their curing reaction for 100 hours
at room temperature to cause the surface layer of the matrix resin layer 2 to be weakly
hardened. Thus, the high viscosity layer 2a having a viscosity of 2,000,000 to 5,000,000
mPa.s is formed as the surface layer.
[0031] Thereafter, the cover film 3 supplied from a film roller 16 is applied to the prepreg
to make it a product.
[0032] The cover film 3 may be, for example, films of such thermoplastic resins as polyethylene,
polypropyrene, polyethylene terephthalate, polyvinyl chloride, polycarbonate, polyvinylidene
chloride, ethyl cllulose, cellulose acetate, etc. The thickness of the cover film
3 is about 5 to 100 µm.
[0033] As for the release papers 1 and 5, papers having releasability may be empolyed as
usual. Although the thickness of the paper depends on the thickness of the matrix
resin layer, the thickness of the paper preferably is about 20 to 200 µm.
[0034] According to the present invention, the prepreg is manufactured by the method described
above such that the furface layer of the matrix resin layer 2 with the reinforcing
fibers 4 is the high viscosity layer 2a. Thus, the cover film laid over the surface
layer does not adhere to the same. Therefore, after easily separating the cover film
3 from the prepreg, the prepreg can be supplied for manufacturing fiber reinforced
composite articles. As the high viscosity layer 2a is formed by applying the room-temperature
curing type hardner 6 onto the matrix resin layer composed of the low viscosity matrix
resin 2', the formation of the high viscosity layer 2 is easy.
[0035] Fig. 3 is an explanatory view showing another embodiment of the prepreg manufacturing
metohd according to the present invention. This embodiment is characterized in that,
in the embodiment as shown in Fig. 1, the second release paper 5 is also coated with
the matrix resin 2' by means of a similar roll coater 10.
[0036] A prepreg is manufactured by a method corresponding to the embodiment as shown in
Fig. 1. Namely, a first and a second release papers 1 and 2 each having the marix
resin layer 2 formed with the resin 2' is fed in between a pair of press rollers 11.
Concurrently with this, reinforcing fibers 4 are successively supplied in the longitudinal
direction of the fibers from a fiber supply roller not shown, into the pair of press
rollers 11 covering the width of the release papers 1 and 5 so that the reinforcing
fibers 4 are disposed between the matrix resin layers while arranging the fibers in
one direction. Subsequently, after pressing the reinforcing fibers 4 and the matrix
resin layer 2 together, the reinforcing fibers 4 are forced into the matrix resin
layer to impregnate the fibers 4 with the matrix resin 2' by pressing and heating
the reinforcing fibers 4 and the matrix resin layer 2 from the upper and the lower
sides thereof. Simultaneously, the resin 2' is partially cured to thereby obtain a
unidirectional fiber reinforced prepreg.
[0037] The method then continues as described above. Namely, after separating one of the
release papers, for instance, the second release paper 5 by the take-up roller 14,
the room-temperature curing type hardener 6 is coated on the prepreg by means of the
spray coater 15 downstream of the separation section. The surface layer of the matrix
resin layer 2 is weakly cured to form the high viscosity layer 2a. Then, the cover
film supplied from the film roller 16 is laid over the prepreg to make it a product,
as previously shown in Fig. 2. This embodiment can provide the prepreg to which the
cover film 3 does not adhere, and attain similar effects.
[0038] Fig. 4 is an explanatory view showing a further embodiment of the prepreg manufacturing
metohd according to the present invention. This embodiment is characterized in that,
in the embodiment as shown in Fig. 1, a resin-coated paper 20 on which the low viscosity
matrix resin 2' has been coated previously on a release paper 21 is substituted for
the first release paper 1 which is supplied to the manufacuring process while being
coated with the matrix resin 2'.
[0039] The resin coated paper 20 is fed in between the pair of press rollers 11 after a
cover film 17, which is laid over the matrix resin layer composed of the resin 2',
is separated by means of a take-up roller 18. After that, similar processes to those
of the embodiment of Fig. 1 are conducted. In Fig. 4, the same reference numerals
as those given in Fig. 1 denote the same members.
[0040] This embodiment can produce a prepreg to which the cover film 3 does not adhere and
attain similar effects.
[0041] The embodiments of the present invention will be further described by the Examples
given hereinafter.
Example 1
[0042] In accordance with the present invention, the prepreg as shown in Fig. 2 was manufactured
by the method as shown in Fig. 3.
[0043] As regards the first and the second release papers 1 and 5, release papers each having
a thickness of 120 µm were used. An epoxy resin (manufactured by Petrochemical Shell
Co. Ltd.) as the matrix resin 2' was coated each of the release papers 1 and 5 by
the respective roll coaters 10. The resin temperature during coating was 80°C while
the coating weight of coated resin was 40 g/m². Dicyandiamide (DICY) as the curing
agent was previously added to the epoxy resin. The content of addition was 40 mg/g
with respect to the epoxy resin. This caused the curing temperature of the epoxy resin
to be 130°C and the viscosity during coating to be 2,000 mPa.s at a resin temperature
of 70°C. A low viscosity epoxy resin layer having a uniform thickness was formed on
the release papers 1 and 5.
[0044] The reinforcing fibers 4 were supplied in between two sheets of the matrix resin
coated release papers 1 and 5 while arranging the fibers 4 in one direction. The fibers
4 and the release papers 1 and 5 were then pressed together by means of the press
roller 11. As regards the reinforcing fibers 4, pitch based carbon fibers each having
a diameter of 10 µm ("FT700 3K" manufactured by Tonen Corporation) were employed.
The reinforcing fibers were arranged in one direction along the length of the fibers
in between the epoxy resin layers of the release papers 1 and 5 at a fiber arrangement
rate of 3 fibers per unit length (cm) in the direction of the width of the release
papers.
[0045] After being pressed by the rollers 11, the reinforcing fibers and the release papers
were heated at 80°C by the hot plate 13 and concurrently pressed by the press roller
12 at the pressing and heating section such that the epoxy resin was impregnated into
the carbon fibers and partially cured ("B stage").
[0046] After the second release paper 5 was separated, polyamideamine (manufactured by Fuji
Kasei K.K.) as the room-temperature curing type hardener 6 was coated on the epoxy
resin layer with the reinforcing fibers 4 at a rate of 0.4g per square metre by means
of the spray coater 15. The curing reaction by the hardner was completed in 4 days.
As a result, the surface layer of the epoxy resin layer was slightly reacted to make
the viscosity as high as 3,000,000 mPa.s whereby the high viscosity layer 2a was formed
on the surface layer to thereby obtain a unidirectional carbon fiber reinfdrced prepreg.
[0047] Subsequently, a polyethylene resin film as the dover film 3 was laid over the prepreg
to make it a prepreg product.
[0048] As a result, the cover film 3 formed of the polyethylene resin film did not adhere
to the epoxy resin layer with the reinforcing fibers. Therefore, the cover film 3
was satisfactorily separated from the resin layer, so that the prepreg was able to
be used for manufacturing composite materials.
Comparative Example 1
[0049] In Example 1, the room-temperature curing type hardner 6 was not coated on the epoxy
resin layer after the epoxy resin layer with the reinforcing fibers was partially
cured. Thus, the epoxy resin layer had a low viscosity of 1,000,000 mPa.s at 23°C.
Otherwise, the same procedure as in Example 1 was followed to manufacture a prepreg.
[0050] As a result, in the obtained prepreg, it was difficult to separate the cover film
formed of the polyethylene resin film since the cover film adhered to the epoxy resin
layer.
[0051] As described above, according to the present method, the matrix resin is impregnated
into the reinforcing fibers and partially cured, and then the room-temperature curing
type hardener is coated on the matrix resin layer with the reinforcing fibers wherby
the matrix resin layer is weakly cured to make the viscosity of the surface layer
of the matrix resin layer high. Therefore, even if there is employed such a low viscosity
matrix resin that the matrix resin layer is sticky due to the low viscosity after
being partially cured, such stickiness of the matrix resin layer with the reinforcing
is removed. As a result , there is provided a prepreg which can prevent the cover
film from adhering thereto. Accordingly, it is possible to easily separate the cover
film from the prepreg and to employ the prepreg for producing fiber reinforced composite
materials. Moreover, as the low viscosity matrix resin is employed, the reinforcing
fibers are sufficiently and uniformly impregnated with the matrix resin, resulting
in producing a prepreg of good quality.
1. A method of manufacturing a prepreg comprising:
coating a release paper with a matrix resin having a low viscosity;
supplying reinforcing fibers in between said release paper coated with the matrix
resin and a release paper which is not coated with the matrix resin;
impregnating said reinforcing fibers with the matrix resin by heating and pressing
the release papers while arranging the reinforcing fibers on the matrix resin layer;
separating one of the papers;
subsequently, applying a room-temperature curing type hardener onto a surface of
the matrix resin layer to weakly harden the surface layer of the matrix resin layer;
and
thereafter, covering said matrix resin layer with a cover film.
2. A method of manufacturing a prepreg comprising:
coating a first and a second release papers with a matrix resin having a low viscosity;
supplying reinforcing fibers in between said release papers coated with the matrix
resin;
impregnating said reinforcing fibers with the matrix resin by heating and pressing
the release papers while arranging the reinforcing fibers between the matrix resin
layers;
separating one of the papers;
subsequently, applying a room-temperature curing type hardener onto a surface of
the matrix resin layer and then to weakly harden the surface layer of the matrix resin
layer; and
thereafter, covering said matrix resin layer with a cover film.
3. The method of manufacturing a prepreg according to claim 1 or claim 2, wherein said
matrix resin is a thermosetting matrix resin such as an epoxy resin, an unsaturated
polyester resin, a polyurethane resin, a diallyl phthalate resin, and a phenolic resin.
4. The method of manufacturing a prepreg according to claim 1 or claim 2, wherein said
room-temperature curing type hardener is aromatic amine or polyamine.
5. The method of manufacturing a prepreg according to claim 1 or claim 2, wherein said
weakly hardened surface layer of the matrix resin layer has a viscosity of 2,000,000
to 5,000,000 cp.
6. The method of manufacturing a prepreg according to claim 1 or claim 2, wherein said
reinforcing fibers are at least one kind of the fibers selected from inorganic fibers
such as carbon fibers, boron fibers, glass fibers, alumina fibers, silicon carbide
fibers and silicon nitride fibers; organic fibers such as aramid fibers, polyarylate
fibers and polyethylene fibers; or metal fibers such as titanium fibers, amorphous
fibers and stainless steel fibers.
7. The method of manufacturing a prepreg according to claim 1 or claim 2, wherein said
cover film is of such a thermoplastics resin as polyethylene, polypropyrene, polyethylene
terephthalate, polyvinyl chloride, polycarbonate, polyvinylidene chloride, ethyl cellulose
or cellulose acetate.
8. The method of manufacturing a prepreg according to claim 1 or 2, wherein instead of
using said release paper while coating the paper with the low viscosity matrix resin,
a resin-coated paper, in which a low viscosity matrix resin layer was formed on a
release paper in advance, is used.
9. A prepreg made by the method according to any of claim 1 to 8, and a fiber reinforced
composite article moulded therefrom.